This paper discusses the potential use of hydrogen peroxide as oxidizer for solid rocket
propulsion. While hydrogen peroxide is a liquid in normal conditions, it may be used in solid …

This paper presents the topic of using solid rocket propulsion for de-orbiting spacecraft, in
order to fulfil space debris mitigation requirements. The benefits and disadvantages of using …

The proliferation of debris in Low Earth Orbit raises increasing challenges about the
sustainability of the space environment. The current international recommendations to …

This chapter presents the topic of low-burn-rate composite solid rocket propellants. While the
majority of presently developed systems require high burn rates, several applications benefit …

Low-thrust, end-burning solid rocket motors have applications as propulsion systems for a
class of small, transonic, uncrewed aerial vehicles. This paper provides new experimental …

Small, low-thrust, long-burn-time solid propellant rocket motors could provide propulsion for
a new class of kilogram-scale, transonic, uncrewed aerial vehicles (UAVs). This paper …

Low-thrust long-burn-time solid rocket motors may be useful as propulsion for small, fast,
uncrewed aerial vehicles. These motors require a slow-burning propellant that can operate …